| Type | Helicopter | |
| Company | Cessna Aircraft Company | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
9.0
88.7
|
fuselage length |
|
1.9
13.0
88.7
|
overall length | |
| Height (m) |
0.6
2.5
50.1
|
|
| Rotors | ||
| Disc area (m2) |
1.4
89.4
460
|
|
| Main rotor diameter (m) |
1.2
10.7
62
|
|
| Tail rotor diameter (m) |
0.8
1.3
4.9
|
|
| Weights | ||
| Empty weight (kg) |
8
943.5
276,800
|
|
| Loaded weight (kg) |
5
1,406.1
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Capacity passengers (per.) |
1
3
400
|
|
| Speeds | ||
| Ground Speed (km/h) |
96.6
173.8
1,500
|
|
| Сruise Speed (km/h) |
52
160
3,087
|
|
| Power | ||
| Total Power (hp) |
0.4
270
60,000
|
1 powerplant |
| Performance | ||
| Service ceiling (m) |
0.6
4,500
161,544
|
|
| Static ceiling (m) |
3
2,300
5,485
|
|
| Range (Ferry range) (km) |
4
432
40,700
|
|
| Endurance (h) |
0.0
5.2
150
|
with auxiliary fuel |
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
313.9
36,000
|
at 2400 m |
| Stat | ||
| Price (USD) |
41.5
79,960
750.0 million
|
|
| Introduction | 1953 | |
| First flight | 01.07.1953 | |
